Si对In718合金凝固过程及元素偏析的影响

本文研究了Ｓｉ对Ｉｎ７１８合金凝固过程及元素偏析的影响。结果表明，当Ｓｉ含量升高后，不仅在枝晶或Ｌａｖｅｓ相中偏析程度加剧，而且在枝晶内的浓度也逐渐升高而达到显著水平。Ｓｉ降低Ｎｂ在Ｌａｖｅｓ相中的溶解度，因而促进Ｌａｖｅｓ相的析出，提高Ｌａｖｅｓ相吸收剩余液体的能力，缩小偏析区的面积。分析认为，过分降低Ｓｉ含量对改善合金凝固组织及提高终凝温度的作用不大。     

镉镍电池大功率工作特性研究

介绍对镉镍电池大电流充放电的试验过程，并对试验结果进行分析。结果表明充电倍率增大时，电池充电电压增量增大，充电效率降低，而内阻压降增大。     

润滑气体及箔片材料对气体动压轴承动特性影响分析

为研究润滑气体和弹性箔片材料特性对波箔型气体动压轴承动特性的影响,以Hydresil型波箔气体动压轴承为研究对象,建立气体流动控制方程和波箔弹性变形模型,通过有限差分法求解扰动方程获得动特性系数。数值分析了润滑气体动力粘度(4.2×1064.6×105·s、轴承波箔片材料泊松比(0.150.45和弹性模量(70340GPa对动特性系数的影响规律。结果表明,在偏心率和转速相同情况下,随气体动力粘度升高,动态刚度系数逐渐增大,且主刚度方向增大最为明显,最大可超过50%动态阻尼系数也增大,且x方向增大最为明显,最大可达60%随轴承箔片材料弹性模量的增大,动态刚度系数不断增大,动态阻尼系数在y方向上逐渐增大,在x方向上逐渐减小;轴承箔片材料泊松比对动特性系数影响较小。     

基于模块化分工的产业集群升级——以常州邹区灯具产业集群为例

初具规模的常州邹区灯具产业集群存在着和其他产业集群共通的问题,制约着产业的进一步发展.模块化生产分工方式有利于解决邹区产业集群面临的困难.文章结合邹区灯具产业实态,运用模块化分工生产理论,对邹区灯具产业集群升级问题展开研究,提出促进灯具配件企业成为灯具产业链的专业模块供应企业,培育现有中型灯具企业上规模,吸引国内外灯具企业加入邹区产业集群,加快灯具产业集群园区建设,强化新产品开发、打造自主品牌等对策建议.     

Design and implementation of five-axis transformation function in CNC system

To implement five-axis functions in CNC system, based on domestic system Lan Tian series, an improved design method for the system software structure is proposed in this paper. The numerical control kernel of CNC system is divided into the task layer and the motion layer. A five-axis transformation unit is integrated into the motion layer. After classifying five-axis machines into different types and analyzing their geometry information, the five-axis kinematic library is designed according to the abstract factory pattern. Furthermore, by taking CA spindle- tilting machine as an example, the forward and the inverse kinematic transformations are deduced. Based on the new software architecture and the five-axis kinematic library, algorithms of RTCP （rotation tool center point control） and 3D radius compensation for end-milling are designed and realized. The milling results show that, with five-axis functions based on such software struc- ture, the instructions with respect to the cutter＇s position and orientation can be directly carried out in the CNC system.     

基于NASTRAN节点载荷批处理的编码技术

飞机载荷主要涉及气动载荷、地面载荷、惯性载荷等,载荷的工况也是琐碎繁多,如何将不同工况、不同部件、不同类型的载荷批量化生成利用NASTRAN进行有限元分析的接口文件,是飞机强度分析输入的关键技术。通过特定的载荷编码技术并结合NASTRAN载荷定义的卡片格式,将某型飞机90种严重工况下的气动节点载荷、地面节点载荷、惯性节点载荷按照一定编码批处理地导入NASTRAN的bdf文件中,分析和计算表明该方法具有良好的载荷识别性能和准确性以及较高的载荷输入效率。     

民机特情乘务训练模拟软件的设计研究

为提高飞行乘务员在民机飞行过程中处理事故的应对能力,消除因人为因素产生的损失,保证飞行的安全性,根据2003年中国国际航空公司编制的飞行乘务员培训大纲中关于乘务应急生存训练内容,提炼出了关于乘务应急生存训练的框架,介绍了编制飞行乘务员应急培训所需要培训模拟软件的设计思路,以期为民机的安全飞行提供技术保障支持。     

Robust optimization of aircraft weapon delivery trajectory using probability collectives and meta-modeling

 Conventional trajectory optimization techniques have been challenged by their inability to handle threats with irregular shapes and the tendency to be sensitive to control variations of aircraft. Aiming to overcome these difficulties, this paper presents an alternative approach for trajectory optimization, where the problem is formulated into a parametric optimization of the maneuver variables under a tactics template framework. To reduce the size of the problem, global sensitivity analysis (GSA) is performed to identify the less-influential maneuver variables. The probability collectives (PC) algorithm, which is well-suited to discrete and discontinuous optimization, is applied to solve the trajectory optimization problem. The robustness of the trajectory is assessed through multiple sampling around the chosen values of the maneuver variables. Meta-models based on radius basis function (RBF) are created for evaluations of the means and deviations of the problem objectives and constraints. To guarantee the approximation accuracy, the meta-models are adaptively updated during optimization. The proposed approach is demonstrated on a typical airground attack mission scenario. Results reveal that the proposed approach is capable of generating robust and optimal trajectories with both accuracy and efficiency.     

Approaching control for tethered space robot based on disturbance observer using super twisting law

Approaching control is a key mission for the tethered space robot to perform the task of removing space debris. But the uncertainties of the TSR such as the change of model parameter have an important effect on the approaching mission. Considering the space tether and the attitude of the gripper, the dynamic model of the TSR is derived using Lagrange method. Then a disturbance observer is designed to estimate the uncertainty based on STW control method. Using the disturbance observer, a controller is designed, and the performance is compared with the dynamic inverse controller which turns out that the proposed controller performs better. Numerical simulation validates the feasibility of the proposed controller on the position and attitude tracking of the TSR.